Thrust Reverser Cowl Rack

ABSTRACT

A rack for holding a portion of a thrust reverser. The rack may include a base and a supporting frame disposed perpendicularly with the base. The base and the supporting frame may include a hinge at each location where the base and the supporting frame are coupled together. The rack may also include two supporting poles parallel to the supporting frame. The two supporting poles may be designed such that the portion of the thrust reverser may be mounted onto the two supporting poles.

RELATED APPLICATIONS

This patent application is a continuation of U.S. patent applicationSer. No. 15/293,066, filed 2016 Oct. 13 and titled THRUST REVERSER COWLRACK, which is a divisional of U.S. patent application Ser. No.12/710,137, filed 2010 Feb. 22 and titled THRUST REVERSER COWL RACK,each of which are incorporated herein by reference in their entirety.

FIELD OF THE INVENTION

Implementations of various technologies described herein generallyrelate to a fixture that may be used to hold a core cowl of a thrustreceiver. More specifically, various technologies described hereingenerally relate to a rack for holding a core cowl of a thrust reverserwhile repair or work is being performed on the core cowl.

DESCRIPTION OF THE RELATED ART

The following descriptions and examples do not constitute an admissionas prior art by virtue of their inclusion within this section. Aircrafttypically use thrust reversers to reverse the direction of theaircraft's thrust and create a drag force to oppose the aircraft'smotion. A typical thrust reverser for use with aircraft engines mayinclude two semicircular duct halves known as a cowl. The cowl of thethrust reverser may include an inner or core cowl and an outer cowl. Thecowl may be aerodynamically shaped such that it is narrower at the rearthan at the front.

In order to reverse the direction of the aircraft's thrust, the outercowl of thrust reverser may slide into a position over the core cowl ofthe thrust reverser such that the exhaust from the aircraft's engine isredirected from the back of the aircraft to the front of the aircraft.

As part of a maintenance program for a thrust reverser, inspection orrepair of the inner wall area of the core cowl may be required. Giventhe enormous size and weight of the thrust reverser's core cowl,maintenance on the thrust reverser core cowl's inner wall components istypically performed while the thrust reverser core cowl is lyinghorizontally on the floor. This position may require that a technicianwork underneath the thrust reverser's core cowl while the technician islying on his back.

SUMMARY

Described herein are implementations of various technologies of a rackused to hold a portion of a thrust reverser. In one implementation, therack may include a base and a supporting frame disposed perpendicularlywith the base. The base and the supporting frame may include a hinge ateach location where the base and the supporting frame are coupledtogether. The rack may also include two supporting poles parallel to thesupporting frame. The two supporting poles may be designed such that theportion of the thrust reverser may be mounted onto the two supportingpoles.

In another implementation, the rack may be designed to hold a core cowlof a thrust reverser. Here, the two supporting poles may be designedsuch that the core cowl of the thrust reverser may be mounted onto thetwo supporting poles.

Described herein are also implementations of various techniques forpositioning a core cowl of the thrust reverser in an upright positionusing the rack. The method may include coupling the core cowl to therack. The rack may be positioned such that the supporting frame ishorizontally disposed on a floor. The method may further includerotating the rack such that the base is lying on the floor and thesupporting frame is standing in an upright position.

The above referenced summary section is provided to introduce aselection of concepts in a simplified form that are further describedbelow in the detailed description section. The summary is not intendedto identify key features or essential features of the claimed subjectmatter, nor is it intended to be used to limit the scope of the claimedsubject matter. Furthermore, the claimed subject matter is not limitedto implementations that solve any or all disadvantages noted in any partof this disclosure.

BRIEF DESCRIPTION OF THE DRAWINGS

Implementations of various techniques will hereafter be described withreference to the accompanying drawings. It should be understood,however, that the accompanying drawings illustrate only the variousimplementations described herein and are not meant to limit the scope ofvarious techniques described herein.

FIG. 1 illustrates a perspective view of a thrust reverser core cowlrack and a thrust reverser core cowl in accordance with implementationsof various technologies described herein.

FIG. 2 illustrates a top view of a thrust reverser core cowl rack inaccordance with implementations of various technologies describedherein.

FIG. 3 illustrates a front view of a thrust reverser core cowl rack inaccordance with implementations of various technologies describedherein.

FIG. 4 illustrates a side view of a thrust reverser core cowl rack inaccordance with implementations of various technologies describedherein.

FIG. 5 illustrates a front view of a receptacle on a thrust reversercore cowl in accordance with implementations of various technologiesdescribed herein.

FIG. 6 illustrates a flow diagram of a method for vertically positioninga thrust reverser core cowl using a thrust reverser core cowl rackaccording to one or more implementations of various techniques describedherein.

FIG. 7 illustrates perspective view of a thrust reverser core cowl rackthat has been rotated in accordance with implementations of varioustechnologies described herein.

DETAILED DESCRIPTION

The discussion below is directed to certain specific implementations. Itis to be understood that the discussion below is only for the purpose ofenabling a person with ordinary skill in the art to make and use anysubject matter defined now or later by the patent “claims” found in anyissued patent herein.

The following paragraphs provide a brief description or summary ofvarious technologies and techniques directed at a thrust reverser corecowl rack and for using same to hold a thrust reverser core cowl in avertical position.

The thrust reverser core cowl rack includes a pair of supporting devices(or poles), a pair of hinges, a supporting frame, a base, a balancehoist, a lift hoist and stabilizers. The hinges are used to couple thesupporting frame to the base. The supporting frame and the base arepositioned at ninety degrees to each other. The hinges allow thesupporting frame and the base to rotate around the hinges' axis, whilekeeping the ninety degree angle between each other. The pair ofsupporting devices is positioned above and parallel to the supportingframe. The pair of supporting devices is also horizontally separated bya predetermined distance that is equal to the horizontal distancebetween two receptacles on the thrust reverser core cowl. Thereceptacles on the thrust reverser are typically used to couple an outercowl of the thrust reverser to the core cowl of the thrust reverser. Assuch, the pair of supporting devices is designed to use the receptaclesthat are already on the core cowl of the thrust reverser.

In one implementation, the supporting frame may include a lifting hoistsuch that a crane may be coupled to the supporting frame via the liftinghoist. Similarly, the base may include a balance hoist such that anothercrane may be coupled to the base via the balance hoist. In anotherimplementation, the hinges may include a hydraulic pump that may be usedto push the supporting frame or the base off of the ground and rotatethe thrust reverser core cowl rack ninety degrees.

In operation, the thrust reverser core cowl rack may be initiallypositioned such that its supporting devices are parallel to the floor.The thrust reverser core cowl may then be coupled to the supportingdevices by mounting the receptacles of the thrust reverser core cowlonto the supporting devices. In one implementation, the thrust reversercore cowl may be coupled to the supporting devices by lifting the thrustreverser core cowl and sliding the receptacles of the thrust reversercore cowl onto the supporting devices using a crane.

After the thrust reverser core cowl is coupled to the supportingdevices, one or more stabilizers and fasteners may be used to secure thethrust reverser core cowl to the thrust reverser core cowl rack. Aftersecuring the thrust reverser core cowl to the thrust reverser core cowlrack, a first crane may be coupled to the lifting hoist on the thrustreverser core cowl rack, and a second crane may be coupled to thebalancing hoist on the opposite end of the thrust reverser core cowlrack. The first crane may lift the lifting hoist such that thehorizontal portion of the thrust reverser core cowl rack may be rotatedninety degrees from a horizontal position to a vertical position. Whilethe first crane is lifting the lifting hoist, the second crane may beused to balance the weight of the thrust reverser core cowl. Afterrotating the thrust reverser core cowl rack ninety degrees, the thrustreverser core cowl may be hanging vertically on the supporting devices.Although the thrust reverser core cowl rack has been described as beingrotated using two cranes, it should be noted that in otherimplementations the thrust reverser core cowl rack may be rotated usingthe hydraulic pump instead.

Various implementations of the thrust reverser core cowl rack andvarious techniques for using same to hold a thrust reverser core cowl ina vertical position will now be described in more detail with referenceto FIGS. 1-7 and in the following paragraphs.

FIG. 1 illustrates a perspective view of a thrust reverser core cowlrack 100 and a thrust reverser core cowl 110 in accordance with variousimplementations described herein. The thrust reverser cowl rack 100(e.g., rack 100) may include a pair of supporting devices 120, a pair ofhinges 140, a hydraulic pump 145, a supporting frame 150, a base 160, abalance hoist 170, a balance crane 175, a lift hoist 180 and stabilizers190. FIG. 1 also shows half of a thrust reverser's core cowl 110 (e.g.,cowl 110) to illustrate how the cowl 110 may couple to the rack 100.Additional details as to how the cowl 110 may couple to the rack 100 areprovided below with reference to FIG. 6.

FIG. 1 illustrates the rack 100 in an initial position with thesupporting frame 150 positioned on the floor. The supporting frame 150is coupled to the base 160 such that the angle between the supportingframe 150 and the base 160 is ninety degrees. The supporting frame 150is coupled to the base 160 via the hinges 140. The hinges 140 allow thesupporting frame 150 and the base 160 to rotate together as one unitaround a rotating axis 130, while maintaining the ninety degree anglebetween the supporting frame 150 and the base 160. The rotating axis 130travels through the center of two hinges 140. The hinges 140 may becoupled to the floor in order to stabilize the rack 100.

The supporting frame 150 may include a lifting hoist 180 such that acrane or other lifting device may couple to the lifting hoist 180 andlift the supporting frame 150. The base 160 may include a balance hoist170 such that a crane or other lifting mechanism may provide support tothe base 160 while the supporting frame 150 is being lifted. The balancecrane 175 illustrates how a crane may be coupled to the balance hoist170.

As mentioned above, the rack 100 may include a hydraulic pump 145. Inlieu of or in combination with using the balance crane 175, thehydraulic pump 145 may be used to push the supporting frame 150 off ofthe ground and rotate the rack 100 along the rotating axis 130 until thebase 160 is lying on the floor and the supporting frame 150 is in avertical position.

In the initial position of the rack 100, the supporting devices 120 arepositioned above the supporting frame 150 parallel with the supportingframe 150. The supporting devices 120 are coupled to the base 160 suchthat they may be located above the supporting frame 150 and at apredetermined horizontal distance apart from each other. Thepredetermined horizontal distance is equal to the horizontal distancebetween two receptacles on the cowl 110. In one implementation, thesupporting devices may be shaped as cylindrical poles such that they mayfit into the receptacles on the cowl 110.

Each side of the cowl 110 includes a receptacle such that the supportingdevices 120 may slide into the receptacles of the cowl 110. Thereceptacles on the cowl 110 may be commonly referred to as a T-track.Typically, the receptacles on the cowl 110 are used to couple the outercowl of the thrust reverser to the core cowl (e.g., cowl 110) of thethrust reverser. When used together, the outer cowl may slide across thereceptacles such that the exhaust air coming from the engine isredirected to the front of an aircraft in order to reverse the thrust ofthe aircraft. The receptacles may be cylindrical in shape. Thereceptacles are more clearly shown in FIG. 5, which will be discussed inthe paragraphs below.

The supporting frame 150 may include stabilizers 190 to provide supportbetween the supporting frame 150 and the cowl 110. In oneimplementation, after the cowl 110 is fixed onto the supporting devices120, the stabilizers 190 may be used to support the weight of the cowl110 on the supporting frame 150. The stabilizers 190 may be adjustablein height such that the cowl 110 may be locked into position against thesupporting frame 150. The stabilizers 190 may be coupled to a cross barthat connects the two parallel ends of the supporting frame 150. Thestabilizers 190 may be adjustable such that they may move across thecrossbar and may be fixed at any position along the crossbar.

FIG. 2 illustrates a top view 200 of the thrust reverser core cowl rack100 in accordance with implementations of various techniques describedherein. The following description of the top view 200 of the thrustreverser core cowl rack is made with reference to the perspective viewof a thrust reverser core cowl rack 100 in FIG. 1. Since FIG. 2 providesa top view of the rack 100, the supporting frame 150 is clearlyillustrated. As seen in FIG. 2, the supporting frame 150 consists ofthree outer bars (i.e., outer bar 210 ₁, outer bar 210 ₂ and outer bar210 ₃) that are each coupled with each other such that the angle betweeneach adjacent bar is ninety degrees. In one implementation, the twoparallel outer bars (i.e., outer bar 210 ₁ and outer bar 210 ₃) of thesupporting frame 150 may be coupled together with a cross bar 220.

In one implementation, the cross bar 220 may be parallel to the outerbar 210 ₂. However, it should be noted that in other implementations,the cross bar 220 does not need to be parallel to the outer bar 210 ₂.The supporting frame 150 may also include one or more additional barsthat may be coupled to any of the outer bars 210 or the cross bar 220 inorder to provide structural support for the rack 100. The additionalbars may also provide additional support for the rack 100 such that whenthe cowl 110 is coupled to the rack 100, the structural integrity of therack 100 may not be compromised due to the weight of the cowl 110.

The lift hoist 180, the stabilizers 190, the hinges 140 and the rotatingaxis 130 illustrated in FIG. 2 correspond to the description providedabove with respect to FIG. 1. However, although only one lifting hoist180 and two stabilizers 190 are illustrated in both FIGS. 1 and 2, itshould be noted that in other implementations additional lifting hoists180 and stabilizers 190 may be used. In one implementation, fewer thantwo stabilizers 190 may also be coupled on the cross bar 210.

FIG. 3 illustrates a front view of a thrust reverser core cowl rack inaccordance with implementations of various techniques described herein.The following description of the front view 300 of the thrust reversercore cowl rack 100 is made with reference to the perspective view of thethrust reverser core cowl rack 100 in FIG. 1 and the top view 200 of thethrust reverser core cowl rack 100 in FIG. 2. Since FIG. 3 provides afront view of the rack 100, the base 160 is clearly illustrated. As seenin FIG. 3, the base 160 consists of three outer bars (i.e., bar 310 ₁,bar 310 ₂ and bar 310 ₃) that are each coupled with each other such thatthe angle between each adjacent bar is ninety degrees.

In addition to the outer bars 310, the base 160 may include inner angledbars 320. The inner angled bars 320 may couple two adjacent outer bars310 together. For instance, angled bar 320 ₁ is coupled to outer bar 310₁ and outer bar 310 ₂. Located along each angled bar 320 is a supportingdevice position 330. The supporting device positions 330 indicate pointson the angled bars 320 where the supporting devices 120 may be attached.The distance D between the two supporting device positions 330 maycorrespond to the predetermined distance between the supporting devices120 described above with reference to FIG. 1. In one implementation, thedistance D may be determined based on the thickness of the cowl 110.

Like the supporting frame 150, the base 160 may also include one or moreadditional bars that may be coupled to any of the outer bars 310 or theangled bars 320 to provide structural support for the rack 100. Theadditional bars may also provide additional support for the supportingdevices 120 and the rack 100 such that when the cowl 110 is coupled tothe supporting devices 120, the structural integrity of the supportingdevices 120 or the rack 100 may not be compromised due to the weight ofthe cowl 110.

The balance hoist 170, the stabilizers 190, the hinges 140 and therotating axis 130 illustrated in FIG. 3 correspond to the samedescriptions provided above with respect to FIG. 1. Although only onebalance hoist 170 is illustrated in both FIGS. 1 and 3, it should benoted that in other implementations additional balance hoists 170 may beused.

FIG. 4 illustrates a side view 400 of a thrust reverser core cowl rack100 in accordance with implementations of various techniques describedherein. The following description of the side view 400 of the thrustreverser core cowl rack 100 is made with reference to the perspectiveview of the thrust reverser core cowl rack 100 in FIG. 1, the top view200 of the thrust reverser core cowl rack 100 in FIG. 2 and the frontview 300 of the thrust reverser core cowl rack 100 in FIG. 3. Since FIG.4 provides a side view 400 of the rack 100, FIG. 4 clearly illustrateshow outer bar 210 ₁ and outer bar 310 ₁ (e.g., representative of thesupporting frame 150 and base 160) are coupled together via the hinge140. In FIG. 4, the supporting device 120 is separated from the base 160for illustrative purposes only.

The side view 400 of the rack 100 illustrates a base support bar 410 andsupporting device support bars 420. The base support bar 410 may becoupled to outer bar 210 ₁ of the supporting frame 150 and to outer bar310 ₁ of the base 160 to provide structural support for the rack 100when the cowl 110 is coupled to the supporting devices 120. Similarly, asecond base support bar may be coupled to outer bar 210 ₃ of thesupporting frame 150 and to outer bar 310 ₃ of the base 160 to alsoprovide structural support for the rack 100 when the cowl 110 is coupledto the supporting devices 120.

The thrust reverser core cowl rack 100 may also include supportingdevice support bars 420, such as supporting device support bar 420 ₁,supporting device support bar 420 ₂ and supporting device support bar420 ₃. Supporting device support bar 420 ₁ may be positioned betweenangled bar 320 ₁ and one of the supporting devices 120. Supportingdevice bar 420 ₂ may be positioned between outer bar 310 ₁ and one ofthe supporting devices 120. Supporting device bar 420 ₃ may bepositioned between outer bar 210 ₁ and one of the supporting devices120. The supporting device support bars 420 may be used to providestructural support to the supporting devices 120 such that thesupporting devices 120 may support the weight of the cowl 110 when thecowl 110 is coupled to the supporting devices 120. Although only threesupporting device support bars 420 are illustrated in FIG. 4, it shouldbe noted that in other implementations the number of supporting devicesupport bars 420 may include more support bars or fewer support barsthan the three supporting device support bars 420 that are illustratedin FIG. 4.

FIG. 5 illustrates a front view of a receptacle 510 on a thrust reversercore cowl in accordance with implementations of various technologiesdescribed herein. The following description of the receptacle 510 ismade with reference to the perspective view of the thrust reverser corecowl rack 100 in FIG. 1. The receptacles 510 are located on each side ofthe thrust reverser core cowl. As mentioned above, the receptacles 510on the cowl 110 may be referred to as a T-track and are typically usedto couple the outer cowl of the thrust reverser to the core cowl (e.g.,cowl 110) of the thrust reverser. In this manner, the supporting device120 is designed to have the same shape as the part of the outer cowl ofthe thrust reverser that couples to the receptacle 510. The receptacles510 may extend to a depth such that most of the supporting devices 120may fit within the receptacles 510.

FIG. 6 illustrates a flow diagram of a method 600 for verticallypositioning a thrust reverser core cowl using a thrust reverser corecowl rack 100 according to one or more implementations of varioustechniques described herein. The following description of the flowdiagram of method 600 is made with reference to the thrust reverser cowlrack 100 of FIG. 1, various elements from FIG. 5 and FIG. 7.

At step 610, the rack 100 may be positioned such that the supportingdevices 120 are parallel with the floor. As such, the supporting frame150 may be positioned against the floor.

At step 620, the cowl 110 may be coupled to the rack 100 via thesupporting devices 120. In one implementation, in order to couple thecowl 110 to the rack 100, the cowl 110 may first be lifted using a craneand positioned in front of the supporting devices 120 such that thefront of the cowl 110 is facing the supporting devices 120. Thereceptacles 510 on each side of the cowl 110 may then be mounted ontothe supporting devices 120. After the cowl 110 is mounted on thesupporting devices 120 via the receptacles 510, the stabilizers 190 maybe positioned to keep the cowl 110 stable. The height of the stabilizers190 may be adjusted. In one implementation, fasteners may also becoupled between the supporting frame 150 and the inside of the cowl 110to provide additional support to stabilize the cowl 110.

At step 630, the rack 100 may be rotated ninety degrees such that thesupporting frame 150 moves from a horizontal position to a verticalposition. In one implementation, in order to rotate the rack 100, afirst crane (e.g., lifting crane 185 in FIG. 7) may be coupled to thelifting hoist 180 and a second crane (e.g., balance crane 175 in FIG. 1)may be coupled to the balance hoist 170. Once the lifting hoist 180 andthe balance hoist 170 have been coupled to their respective cranes, thefirst crane may lift the supporting frame 150 by lifting the liftinghoist 180. At the same time, the second crane may be used to ensure thatthe rack 100 is rotated carefully. In this manner, as the first cranelifts the lifting hoist 180, the second crane may lower the balancehoist 170 to create equal vertical forces on the rack 100. The firstcrane may lift the lifting hoist 180 until the supporting frame 150 andthe supporting devices 120 are in a vertical position. Once the rack 100has been rotated, the base 160 may be in a horizontal position lyingagainst the floor and the supporting frame 150 stands in a verticalposition perpendicular to the floor. As a result of this rotation, thecowl 110 now stands in an upright position. In this position, work maybe performed on the inner wall components of the cowl 110 with fewerhazards and more accuracy than when the cowl 110 is laid horizontally onthe floor.

Although the rack 100 has been described herein as being rotated usingcranes, it should be noted that in other implementations the rack 100may be rotated using the hydraulic pump 145. The hydraulic pump 145 maybe configured to push the supporting frame 150 off of the ground androtate the rack 100 ninety degrees. The hydraulic pump 145 may also beconfigured to provide support on the base 160 while rotating thesupporting frame 150.

FIG. 7 illustrates a thrust reverser core cowl rack that has beenrotated in accordance with implementations of various techniquesdescribed herein. The following description of the thrust reverser corecowl rack 700 is made with reference to the perspective view of thethrust reverser core cowl rack 100 in FIG. 1 and method 600 in FIG. 6.As seen in FIG. 7, the supporting frame 150 has been rotated from ahorizontal position to a vertical position. Consequently, the base 160has now been rotated from a vertical position to a horizontal position.Likewise, because the cowl 110 is attached to the rack 100, the cowl 110has also been rotated from a horizontal position to a vertical positionperpendicular to the floor, i.e., in an upright position.

FIG. 1 illustrates the position of the rack 100 and the cowl 110 in step610 of method 600. After rotating the rack 100 ninety degrees (e.g.,step 630), the rack 100 and the cowl 110 may be positioned asillustrated in FIG. 7. In one implementation, a fastener 710 may couplethe cowl 110 to the supporting frame 150. The fastener 710 may provideadditional support to the cowl 110 to stabilize the cowl 110 while it ismounted on the supporting devices 120. FIG. 7 also illustrates how thelifting crane 185 may be coupled to the lifting hoist 180 and used tolift and rotate the supporting frame 150, as described in step 630 ofmethod 600.

While the foregoing is directed to implementations of various techniquesdescribed herein, other and further implementations may be devisedwithout departing from the basic scope thereof, which may be determinedby the claims that follow. Although the subject matter has beendescribed in language specific to structural features and/ormethodological acts, it is to be understood that the subject matterdefined in the appended claims is not necessarily limited to thespecific features or acts described above. Rather, the specific featuresand acts described above are disclosed as example forms of implementingthe claims.

What is claimed is:
 1. A method, comprising: coupling a core cowl of athrust reverser to a rack, wherein the rack comprises: a base; asupporting frame perpendicular to the base; and supporting poles ontowhich the core cowl is to be mounted, wherein the supporting poles arecoupled to the base and parallel to the supporting frame, and whereinthe supporting poles are configured to be inserted into the core cowl;and positioning the core cowl in an upright position.
 2. The method ofclaim 1, wherein positioning the core cowl comprises rotating thesupporting frame and the base together as one unit such that the corecowl is positioned in the upright position.
 3. The method of claim 2,wherein the rack further comprises: one or more hinges.
 4. The method ofclaim 3, wherein the base and the supporting frame are coupled via theone or more hinges.
 5. The method of claim 3, wherein the supportingframe the base are rotated together as one unit around an axis of theone or more hinges such that the core cowl is positioned in the uprightposition.
 6. The method of claim 2, wherein rotating the supportingframe and the base comprises rotating the supporting frame and the baseusing one or more cranes.
 7. The method of claim 2, wherein rotating thesupporting frame and the base comprises rotating the supporting frameand the base using a hydraulic pump.
 8. The method of claim 2, whereinrotating the supporting frame and the base comprises rotating thesupporting frame and the base about ninety degrees.
 9. The method ofclaim 1, wherein the supporting frame is horizontally disposed on afloor.
 10. The method of claim 9, wherein coupling the core cowl to therack comprises: positioning the supporting frame of the rackhorizontally on the floor; and mounting the core cowl onto thesupporting poles.
 11. The method of claim 10, wherein mounting the corecowl comprises mounting one or more receptacles of the core cowl ontothe supporting poles.
 12. The method of claim 10, wherein positioningthe core cowl comprises rotating the supporting frame and the base suchthat the supporting poles hold the core cowl in the upright position.13. The method of claim 1, further comprising: coupling stabilizersdisposed on the supporting frame to the core cowl to facilitate holdingthe core cowl in the upright position.
 14. A system, comprising: athrust reverser; and a rack, comprising: a base; a supporting frameperpendicular to the base; and supporting poles onto which the core cowlis to be mounted, the supporting poles being: coupled to the base andparallel to the supporting frame; and configured to be inserted into thecore cowl.
 15. The system of claim 14, further comprising: one or morehinges, wherein the base and the supporting frame are coupled via theone or more hinges.
 16. The system of claim 15, wherein the supportingframe and the base rotate together as one unit around an axis of the oneor more hinges.
 17. The system of claim 15, further comprising ahydraulic pump disposed proximate a hinge of the one or more hinges tofacilitate rotation of the rack about the axis of the one or morehinges.
 18. The system of claim 14, further comprising: a cross barconnecting two ends of the supporting frame; and one or more stabilizerscoupled to the cross bar and configured to assist the supporting polesin supporting a weight of a portion of the thrust reverser.
 19. Thesystem of claim 14, further comprising a hoist coupled to the supportingframe, wherein the hoist facilitates a crane to lift the supportingframe.
 20. The system of claim 14, further comprising a hoist coupled tothe base, wherein the hoist facilitates a crane to lift the base.